Reduction of Axial Turbomachinery Tonal Noise by Means of Flow Induced Secondary Sources Using an Extremum-Seeking Control Technique

Author:

Lemke O.1,Becker R.2,Neise W.3,King R.2,Möser M.4

Affiliation:

1. Technische Universität Berlin, Sonderforschungsbereich 557, Müller-Breslau-Straße 8, 10623 Berlin, Germany

2. Technische Universität Berlin, Institut für Prozess- und Anlagentechnik, Hardenbergstraße 36a, 10623 Berlin, Germany

3. Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Institut für Antriebstechnik, Abteilung Triebwerksakustik, Müller-Breslau-Straße 8, 10623 Berlin, Germany

4. Technische Universität Berlin, Institut für Strömungsmechanik und Technische Akustik, Einsteinufer 25, 10587 Berlin, Germany

Abstract

In conventional active noise control experiments, loudspeakers are used to generate the secondary anti-phase sound field to be superimposed destructively with the sound waves radiated from the primary source. In the present study, aerodynamic sound sources are used to actively control the tonal noise of an axial fan. This is achieved by disturbing the flow field around the blade tips in such a way that additional periodic forces are set up which in turn form the secondary sound sources. To disturb the flow, air is blown into the blade tip region through the casing wall. The resulting aerodynamic sound sources are adjustable in both amplitude and phase. Results for closed loop control of the blade passing frequency using an extremum-seeking control technique are presented.

Publisher

SAGE Publications

Subject

Acoustics and Ultrasonics,Aerospace Engineering

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